DE2025834C2 - Rotor für ein Drehflügelflugzeug - Google Patents
Rotor für ein DrehflügelflugzeugInfo
- Publication number
- DE2025834C2 DE2025834C2 DE2025834A DE2025834A DE2025834C2 DE 2025834 C2 DE2025834 C2 DE 2025834C2 DE 2025834 A DE2025834 A DE 2025834A DE 2025834 A DE2025834 A DE 2025834A DE 2025834 C2 DE2025834 C2 DE 2025834C2
- Authority
- DE
- Germany
- Prior art keywords
- rotor
- blade
- hub
- components
- fork
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 210000000056 organ Anatomy 0.000 claims description 7
- 239000000314 lubricant Substances 0.000 claims description 3
- 230000001419 dependent effect Effects 0.000 claims 1
- 238000012423 maintenance Methods 0.000 claims 1
- 230000000149 penetrating effect Effects 0.000 claims 1
- 238000007789 sealing Methods 0.000 claims 1
- 239000000725 suspension Substances 0.000 claims 1
- 210000002445 nipple Anatomy 0.000 description 4
- 239000004519 grease Substances 0.000 description 3
- 238000005461 lubrication Methods 0.000 description 2
- 238000004873 anchoring Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/322—Blade travel limiting devices, e.g. droop stops
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/327—Retention means relieving the stress from the arm, e.g. tie-bars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/37—Rotors having articulated joints
- B64C27/39—Rotors having articulated joints with individually articulated blades, i.e. with flapping or drag hinges
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
- Centrifugal Separators (AREA)
- Earth Drilling (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR6917323A FR2041762B1 (enrdf_load_stackoverflow) | 1969-05-28 | 1969-05-28 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE2025834A1 DE2025834A1 (de) | 1970-12-10 |
DE2025834C2 true DE2025834C2 (de) | 1984-06-14 |
Family
ID=9034686
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE2025834A Expired DE2025834C2 (de) | 1969-05-28 | 1970-05-27 | Rotor für ein Drehflügelflugzeug |
Country Status (5)
Country | Link |
---|---|
US (1) | US3679322A (enrdf_load_stackoverflow) |
JP (1) | JPS4818796B1 (enrdf_load_stackoverflow) |
DE (1) | DE2025834C2 (enrdf_load_stackoverflow) |
FR (1) | FR2041762B1 (enrdf_load_stackoverflow) |
GB (1) | GB1314417A (enrdf_load_stackoverflow) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2092720B1 (enrdf_load_stackoverflow) * | 1970-06-11 | 1974-07-12 | Scemm | |
DE2150741C3 (de) * | 1971-10-12 | 1973-11-22 | Messerschmitt Boelkow Blohm | Schlag- und schwenkgelenklose Aufhaengung der Rotorblaetter eines Drehfluegelflugzeuges am Rotorkopf |
US3853426A (en) * | 1972-09-05 | 1974-12-10 | United Aircraft Corp | Elastomeric helicopter rotor head with dynamic and static blade coning and droop stops |
US3778189A (en) * | 1972-09-05 | 1973-12-11 | United Aircraft Corp | Elastomeric helicopter rotor head with dynamic and static blade coning and droop stops |
US3932059A (en) * | 1975-01-10 | 1976-01-13 | United Technologies Corporation | Droop stops for helicopter rotor having elastomeric bearings |
FR2434079A1 (fr) * | 1978-08-23 | 1980-03-21 | Aerospatiale | Dispositif pour limiter les battements des pales d'un rotor principal de giravion |
US4778340A (en) * | 1985-11-25 | 1988-10-18 | Costruzioni Aeronautiche Giovanni Augusta S.P.A. | Main helicopter rotor |
JPH0162003U (enrdf_load_stackoverflow) * | 1987-10-14 | 1989-04-20 | ||
FR2725687B1 (fr) * | 1994-10-12 | 1996-12-27 | Eurocopter France | Dispositif de butees de battement, a anneau escamotable de butees hautes, et tete de rotor le comportant |
CN107089326A (zh) * | 2017-05-12 | 2017-08-25 | 常州银鹰航空科技有限公司 | 一种冗余式挥舞铰旋翼头 |
CN112611535A (zh) * | 2020-11-20 | 2021-04-06 | 惠阳航空螺旋桨有限责任公司 | 一种桨毂支撑定位结构 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB376975A (en) * | 1931-04-24 | 1932-07-21 | Cierva Juan De La | Improvements in aircraft-sustaining rotors |
US2511687A (en) * | 1941-12-29 | 1950-06-13 | Edward F Andrews | Rotor blade lift control for rotary wing sustained aircraft |
GB634529A (en) * | 1942-08-07 | 1950-03-22 | Autogiro Co Of America | Pitch control for aircraft sustaining rotors |
US2614640A (en) * | 1951-02-01 | 1952-10-21 | United Aircraft Corp | Rotor blade support |
US2672941A (en) * | 1951-10-04 | 1954-03-23 | Mcculloch Motors Corp | Means for connecting rotor blades to rotor bodies |
GB1045723A (en) * | 1961-11-06 | 1966-10-19 | Bendix Corp | Improvements in or relating to force transmitting members |
US3147810A (en) * | 1962-09-12 | 1964-09-08 | Boeing Co | Restraining mechanism |
US3200887A (en) * | 1963-08-09 | 1965-08-17 | Enstrom Corp | Helicopter rotor system having elastomeric bearings |
DE1245749B (de) * | 1964-04-24 | 1967-07-27 | Bendix Corp | Verbindungselement fuer den Rotorblattanschluss eines Hubschraubers |
FR1419635A (fr) * | 1964-06-15 | 1965-12-03 | Sud Aviation | Perfectionnement apporté aux mâts de rotor pour hélicoptères |
US3232349A (en) * | 1964-12-02 | 1966-02-01 | Enstrom Corp | Rotor system utilizing centrifugal deflection of non-radial blades |
US3520637A (en) * | 1969-07-24 | 1970-07-14 | Boeing Co | Torsion-tension coupling |
-
1969
- 1969-05-28 FR FR6917323A patent/FR2041762B1/fr not_active Expired
-
1970
- 1970-05-27 DE DE2025834A patent/DE2025834C2/de not_active Expired
- 1970-05-27 GB GB2538070A patent/GB1314417A/en not_active Expired
- 1970-05-27 US US40823A patent/US3679322A/en not_active Expired - Lifetime
- 1970-05-27 JP JP45044933A patent/JPS4818796B1/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
JPS4818796B1 (enrdf_load_stackoverflow) | 1973-06-08 |
FR2041762B1 (enrdf_load_stackoverflow) | 1973-11-16 |
FR2041762A1 (enrdf_load_stackoverflow) | 1971-02-05 |
DE2025834A1 (de) | 1970-12-10 |
GB1314417A (en) | 1973-04-26 |
US3679322A (en) | 1972-07-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8181 | Inventor (new situation) |
Free format text: MOULLLE, RENE LOUIS, AIX-EN-PROVENCE, BOUCHES-DU-RHONE, FR |
|
D2 | Grant after examination | ||
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |